LAX04LA005
2003-10-07 · Jean, Nevada, United States · None · 1 aircraft · Status: Completed
Airport 0L7
Current FAA registration · N3904D
- Make / Model
- CESSNA 182A
- Seats / Engines
- 4 seats · 1 engine
- ADS-B equipped
- Yes — Mode-S A485B1
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's inadequate in-flight planning/decision which resulted in fuel exhaustion and the loss of engine power.
Factual narrative
On October 7, 2003, about 1330 Pacific daylight time, a Cessna 182A, N3904D, nosed over during an off airport forced landing 7 miles southwest of Jean, Nevada. The forced landing was precipitated by a loss of engine power. The airplane was being repositioned to Jean by the pilot for the owner under the provisions of 14 CFR Part 91. The commercial pilot and one passenger were not injured, and the airplane was substantially damaged. The personal cross-country flight departed Lake Elsinore, California, at 1155. Visual meteorological conditions prevailed, and a flight plan had not been filed. The pilot stated to the National Transportation Safety Board investigator that he started a decent out of 9,500 feet mean sea level (msl) when the airplane experienced some moderate turbulence. This was followed by an uncommanded reduction of engine power towards idle. The pilot applied carburetor heat and adjusted the fuel mixture. Despite the pilot's manipulation of engine controls, power was not restored. The pilot selected what appeared to him to be a dirt road on which to force land the airplane. While landing the airplane, deep ruts in the road affected the landing and the airplane came to rest inverted. Examination of the airplane by a Federal Aviation Administration (FAA) inspector found that the total fuel onboard after the accident was 3 gallons. Normal unusable fuel for each tank is 1.5 gallons. However, if the aircraft is not in a level flight attitude, an additional 3.5 gallons of fuel per tank may be unusable due to the aft placement of the fuel line ports in the fuel cells. Following a loss of engine power, the airplane nosed over when the pilot executed a forced landing onto a dirt road. The pilot started a descent out of 9,500 feet mean sea level (msl) when the airplane experienced some moderate turbulence. This was followed by an uncommanded reduction of engine power towards idle. The pilot applied carburetor heat and adjusted the fuel mixture. Despite the pilot's manipulation of engine controls, power was not restored. The pilot selected what appeared to him to be a dirt road on which to force land the airplane. While landing the airplane, deep ruts in the road affected the landing and the airplane came to rest inverted. Examination of the airplane revealed that the total fuel onboard after the accident was 3 gallons. Normal unusable fuel for each tank is 1.5 gallons. However, if the aircraft is not in a level flight attitude, an additional 3.5 gallons of fuel per tank may be unusable due to the aft placement of the fuel line ports in the fuel cells. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_LAX04LA005.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion, turbulence). All research papers
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- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
- arXiv 2024 · arXiv preprint Does small-scale turbulence matter for ice growth in mixed-phase clouds?
Representing the glaciation of mixed-phase clouds in terms of the Wegener-Bergeron-Findeisen process is a challenge for many weather and climate models, which tend to overestimate this process because…
- arXiv 2023 · arXiv preprint Effects of electrostatic interaction on clustering and collision of bidispersed inertial particles in homogeneous and isotropic turbulence
In sandstorms and thunderclouds, turbulence-induced collisions between solid particles and ice crystals lead to inevitable triboelectrification.
- SKYbrary (Eurocontrol) 2023 · SKYbrary article Wake Vortex Turbulence — SKYbrary Knowledge Base
SKYbrary wake vortex turbulence comprehensive article — generation mechanics, dissipation factors, separation standards (ICAO LIGHT/MEDIUM/HEAVY/SUPER + recategorisation RECAT-EU).